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March 1, 2021 · Bell APT70 · N314AQ

Fort Benning, GA

Overview

Report Status
Probable Cause
Event Type
Accident
Date
March 1, 2021
Location
Fort Benning, GA
Aircraft
Bell APT70 (2020)
Tail Number
N314AQ
Operator
Bell Helicopter Textron
Injuries
None
Aircraft Damage
Substantial
NTSB Number
DCA21LA094

According to the operator/manufacturer, the flight was a demonstration for a component of the U.S. Army in a remote area on the grounds of Fort Benning, Georgia. The APT-70 is an unmanned aircraft with vertical take-off and landing (VTOL) capability. Takeoff and landing is conducted in a “tail-sitter” configuration and lifts off with four quad-rotor propellors providing powered lift. The aircraft transitions to forward flight using the propellors for thrust, and a bi-wing configuration for lift. During the flight, the Electronic Speed Controller (ESC) on the number 1 motor faulted, resulting in a loss of thrust from that motor. The aircraft flight controller automatically reduced thrust on the opposite motor to maintain stable attitude control, which caused an overall reduction in thrust and led to a descent and to impact with trees. The aircraft was substantially damaged and there were no injuries. The aircraft is capable of entering a hover and controlled descent in the event of a failed motor; however, this maneuver requires crew action. The impact with the trees occurred about 5 seconds after the failure, before the pilot could take action. The operator/manufacturer identified an ambiguous paragraph in their safety checklist regarding the appropriate response to ESC failure. The examination of flight data and the ESC by the operator/manufacturer identified a cracked ceramic capacitor in the ESC circuitry.

NTSB Probable Cause

failure of an electronic speed controller that resulted in a descent and impact with trees.

Full Narrative

According to the operator/manufacturer, the flight was a demonstration for a component of the U.S. Army in a remote area on the grounds of Fort Benning, Georgia. The APT-70 is an unmanned aircraft with vertical take-off and landing (VTOL) capability. Takeoff and landing is conducted in a “tail-sitter” configuration and lifts off with four quad-rotor propellors providing powered lift. The aircraft transitions to forward flight using the propellors for thrust, and a bi-wing configuration for lift. During the flight, the Electronic Speed Controller (ESC) on the number 1 motor faulted, resulting in a loss of thrust from that motor. The aircraft flight controller automatically reduced thrust on the opposite motor to maintain stable attitude control, which caused an overall reduction in thrust and led to a descent and to impact with trees. The aircraft was substantially damaged and there were no injuries. The aircraft is capable of entering a hover and controlled descent in the event of a failed motor; however, this maneuver requires crew action. The impact with the trees occurred about 5 seconds after the failure, before the pilot could take action. The operator/manufacturer identified an ambiguous paragraph in their safety checklist regarding the appropriate response to ESC failure. The examination of flight data and the ESC by the operator/manufacturer identified a cracked ceramic capacitor in the ESC circuitry.

Flight

Event TypeAccident
Event Time17:00 EST
Nearest Airport0nm
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell APT70
Tail NumberN314AQ
Aircraft CategoryPlft
DamageSubstantial
OperatorBell Helicopter Textron
Engines4
Engine TypeElectric
Engine DetailsHacker · Electric | Hacker · Electric | Hacker · Electric
Seats0

People & Injuries

Fatal0
Serious0
Minor0
Uninjured0
Total0
Crew 1Age 31 · Unknown · None

Conditions

ConditionsVMC
LightDaylight
Wind333° @ 5 kt
Visibility6 sm
CeilingOvercast 7000 ft
Temperature / Dew Point64 F / 0 C
Altimeter0
Observation Time17:00
Weather SourceWFAC

Appendix: Source Data